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2840-01-419-5846
Aircraft Gas Turbine Engine Combustion Chamber
2840014195846 014195846 869082-5
The portion of an ENGINE, GAS TURBINE, AIRCRAFT in which fuel is burned. It may be an annular type in which the space between the circular inner and outer cylinders form the burning chamber or it may be the multi-arrangement can type in which separate can like burn cylinders are positioned in a circular arrangement within an inner and outer case. View more Aircraft Gas Turbine Engine Combustion Chamber
January 2023
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United States (US) 4. 2840-01-419-5846 Marketplace Restrictions Approved Sources Datasheet Management
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869082 https https//www.nsnlookup.com /fsg-28/fsc-2840/us 2840-01-419-5846 2840014195846 014195846,869082
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Restrictions 2840-01-419-5846
2840-01-419-5846 is a Aircraft Gas Turbine Engine Combustion Chamber that does not have a nuclear hardened feature or any other critical feature such as tolerance, fit restriction or application. This item is a US Munitions List or Commerce Control List Item which must be destroyed to prevent restoration or repair. Only authorized parties may possess this item. This item is not suspected to be hazardous. This item does not contain a precious metal.
Import and Export 2840-01-419-5846
- Schedule B
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- HTS Code
- Subscribe to View HTS Code
End Users 2840-01-419-5846
- Spain (YB01)
- Effective Date:
- 1 Sep 1995
Approved Sources 2840-01-419-5846
- Part Number
- Manufacturer
- Status
- 869082-5
- Manufacturer
- 99193 - Honeywell International Inc. (Active)
- Primary Buy
- Primary Buy
Datasheet 2840-01-419-5846
- Characteristic
- Specifications
- FIIG
- Specifications
- A530F0
- End Item Identification [AGAV]
- Ppe 31 Turbo Propeller 331
NATO Stock Numbers Related to 2840-01-419-5846
Freight Information 2840-01-419-5846
2840-01-419-5846 has freight characteristics.. 2840-01-419-5846 has a variance between NMFC and UFC when transported by rail and the description should be consulted.